diff --git a/simPrototypeSTART.m b/simPrototypeSTART.m
index cba9664..165366f 100644
--- a/simPrototypeSTART.m
+++ b/simPrototypeSTART.m
@@ -3,17 +3,17 @@ close all; clear all; clc;
 
 %% User Defined Values
 % Initial Conditions
-Kp = -2^3;
-Ki = -2^-2;
-Kd = -2^0.75;
+Kp = -8;
+Ki = -0.25;
+Kd = -1.6818;
 
 v0          = 0;                                                            % Initial Velocity (z)          [m/s]
 M0          = 1.2;                                                          % Initial Mass                  [kg]
 yaw0        = 75;                                                            % Initial Yaw                   [deg]
-pitch0      = 50;                                                            % Initial Pitch                 [deg]
+pitch0      = 0;                                                            % Initial Pitch                 [deg]
 roll0       = 0;                                                            % Initial Roll                  [deg]
 p0          = 0;                                                            % Initial Angular Velocity (x)  [deg/s]
-q0          = 0;                                                            % Initial Angular Velocity (y)  [deg/s]
+q0          = 0;                                % Initial Angular Velocity (y)  [deg/s]
 r0          = 0;                                                            % Initial Angular Velocity (z)  [deg/s]
 
 Tcurve = readmatrix('F15_thrustCurve.txt');                                 % Thrust Curve from .txt        [t, N]
@@ -26,7 +26,7 @@ tb          = Tcurve(end, 1) - Tcurve(1, 1);                                % Bu
 mdot        = Mp / tb;                                                      % Mass Flow Rate                [kg/s]
 D           = 0;                                                            % Drag                          [N]
 stepSize    = 0.001;                                                        % Simulation Step Size          [s]
-maxServo    = 15;                                                           % Max Servo Rotation            [deg]
+maxServo    = 7.5;                                                           % Max Servo Rotation            [deg]
 
 % Moment of Inertia / Mass
 I11         = (1/12) * 0.5318^2 + 0.25 * 0.05105^2;                         % (1/12) * h^2 + 0.25 * r^2